System pressure actuated by=pass valve for servomotor

The control, by-pass valve contains a valve plug (24) axially slidable in a valve housing (22). There is at least one valve spring, acting on the valve plug, in a spring chamber radially widened w.r.t. the valve plug. A two-arm spring bracket element (30) forms the valve spring and has a middle sect...

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Bibliographic Details
Main Author SCHULLER, JOHANNES, 83620 FELDKIRCHEN-WESTERHAM, DE
Format Patent
LanguageEnglish
German
Published 18.01.1996
Edition6
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Abstract The control, by-pass valve contains a valve plug (24) axially slidable in a valve housing (22). There is at least one valve spring, acting on the valve plug, in a spring chamber radially widened w.r.t. the valve plug. A two-arm spring bracket element (30) forms the valve spring and has a middle section, acting on the valve plug. Its arms (36) extend on either side transversely to the valve plug axis. The ends, radially spaced from the valve plug, are fixed to the valve housing.
AbstractList The control, by-pass valve contains a valve plug (24) axially slidable in a valve housing (22). There is at least one valve spring, acting on the valve plug, in a spring chamber radially widened w.r.t. the valve plug. A two-arm spring bracket element (30) forms the valve spring and has a middle section, acting on the valve plug. Its arms (36) extend on either side transversely to the valve plug axis. The ends, radially spaced from the valve plug, are fixed to the valve housing.
Author SCHULLER, JOHANNES, 83620 FELDKIRCHEN-WESTERHAM, DE
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Snippet The control, by-pass valve contains a valve plug (24) axially slidable in a valve housing (22). There is at least one valve spring, acting on the valve plug,...
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SubjectTerms AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Title System pressure actuated by=pass valve for servomotor
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